▸Orbital parameters

Orbit class	SSO
Inclination	97.4717°
Eccentricity	0.0006217
Period	94.8 min
Apogee	514 km
Perigee	505 km
Mean motion	15.18812021 rev/day
RAAN	263.7290°
Arg of perigee	305.4501°
Mean anomaly	54.6153°
B*	3.0164e-4
Rev at epoch	6,239

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 64088U 25108B 26188.15437774 .00006213 00000-0 30164-3 0 9994

2 64088 97.4717 263.7290 0006217 305.4501 54.6153 15.18812021 62399

▸ source OMM (JSON)

{
  "OBJECT_NAME": "2025-108B",
  "OBJECT_ID": "2025-108B",
  "EPOCH": "2026-07-07T03:42:18.237+00:00",
  "MEAN_MOTION": 15.18812021,
  "ECCENTRICITY": 0.0006217,
  "INCLINATION": 97.4717,
  "RA_OF_ASC_NODE": 263.729,
  "ARG_OF_PERICENTER": 305.4501,
  "MEAN_ANOMALY": 54.6153,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 64088,
  "REV_AT_EPOCH": 6239,
  "BSTAR": 0.00030164,
  "MEAN_MOTION_DOT": 0.00006213,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	2025-108B
Operator	Micro-Nano Star Space Technology Co. Ltd.dHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	May 21, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	350HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/64088

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.